发明名称 ACTIVE SYNCHRONIZING RING
摘要 An improved system, apparatus and method for controlling vane angles in a gas turbine engine, and more specifically, for correcting vane angle error in a gas turbine engine. An active synchronization ring comprises a plurality of micro-actuators coupled to the synchronization ring to correct distortion in the synchronization ring. The micro-actuators apply a bending moment to the synchronization ring to cancel or compensate for synchronization ring distortion. The micro-actuators may be controlled open loop or closed loop. Strain sensors measure ring distortion and provide signals to the controller for closed loop control.
申请公布号 US2015184535(A1) 申请公布日期 2015.07.02
申请号 US201414576858 申请日期 2014.12.19
申请人 Rolls-Royce North American Technologies, Inc. 发明人 Dougherty Michael P.
分类号 F01D17/16;F01D9/04 主分类号 F01D17/16
代理机构 代理人
主权项 1. A system for controlling individual vane angles in a gas turbine engine, comprising: a synchronization ring having a plurality of micro-actuators coupled to said synchronization ring, each of said micro-actuators create a bending moment in said synchronization ring, each of said micro-actuators having an input for receiving a control signal; and an actuator pivotally attached to said synchronization ring for rotating said ring about an axis.
地址 Indianapolis IN US